00-306-3108
Structural Component Air Support
Aluminum alloy, qq-a-200/11, 1.953 in. w, 0.188 in. dia hole thru base 4 places
00-306-3514
Structural Component Air Support
Used on acft model c130. 1.000 in.w, 1.920 in.lg, used on liferaft compt door release tube
00-306-3562
Aircraft Window Panel
Used on c-130hercules airplane. 8 mounting holes; holes diameter, 0.325 in. ; 0.333 in.
00-306-3573
Structural Component Air Support
Used on acft model c130. al alloy 356-T6 per qq-a-601 comp 3, used on nose landing gear uplock
00-306-3585
Structural Component Air Support
Used on acft model c130. aluminum alloy sand casting 356-T6 per qq-a-601, bracket-rudder, auto-pilot servo, lower
00-306-3652
Structural Aircraft Panel
00-306-3675
Structural Component Air Support
Used on c-130 acft.
00-306-4017
Structural Component Air Bracket
0.051" material thickness
00-306-4344
Aircraft Door
Used on c-130 aircraft.
00-306-4349
Aircraft Leading Edge
00-306-4402
Aircraft Tip
27.780" overall length u/a: fin tip assy
00-306-4967
Fuel Aircraft Tank
00-306-7502
Aircraft Door
00-306-7533
Aircraft Hinge
00-306-8080
Aircraft Door
Used on aircraft model c54.
00-306-8081
Aircraft Door
Used on aircraft model c54.
00-306-8083
Aircraft Door
Used on C-54.
00-307-0035
Filler Opening Cap
2.375" outside diameter cadmium surface treated
00-307-0787
Access Aircraft Door
00-307-0876
Access Aircraft Cover
Anodize surface treated
00-307-0893
Access Aircraft Door
00-307-1142
Structural Aircraft Plate
00-307-1145
Structural Component Air Support
00-307-1724
Aircraft Windshield Panel
21.850 in.lg; 19.583 in.w; 16 holes, 0.249 in.min, 0.257 in.max dia, 16 holes, 0.341 in.min, 0.349 in.max dia, 27 holes, 0.309 in.min, 0.317 in.max dia;
00-307-1727
Aircraft Windshield Panel
Used on aircraft,c-130.
00-307-1728
Aircraft Windshield Panel
Glass, laminated, 36 holes along outer edge, 0.3125 in.dia;
00-307-1729
Aircraft Windshield Panel
36 holes 0.309 in. min, 0.317 in. max dia
00-307-1730
Aircraft Window Panel
Glass, 52 holes 0.3125 in. dia along outed edge
00-307-1731
Aircraft Window Panel
Used on c-130 aircraft. 52 holes 0.3125 dia along outer edge
00-307-1732
Aircraft Window Panel
Glass, laminated, 54 holes along outer edge, 0.309 in. min, 0.317 in. max dia
00-307-1733
Aircraft Windshield Panel
Appl to c-130 acft;
00-307-1848
Access Aircraft Cover
00-307-1910
Wing Landing Flap
Used on aircraft model c130.
00-307-1922
Structural Component Air Support
Used on acft model c130a. 2.650 in.w, 4.250 in.h, 4.250 in.lg, located at fus sta 814, right hand
00-307-1943
Access Aircraft Door
00-307-1981
Structural Component Air Support
Used on c-130 acft. supports horizontal stabilizer anti-icing ejector assy
00-307-2070
Structural Component Air Support
Used on acft model c130. aluminum alloy per qq-a-601 composition 3
00-307-2317
Aircraft Stiffener
00-307-2391
Aircraft Leading Edge
Matl: alum alloy
00-307-2429
Structural Component Air Bracket
10.125" overall length bracket, oil return
00-307-2780
Filler Opening Cap
4.250" outside diameter pressure fuel servicing
00-307-3073
Structural Component Air Support
Used on support instl p/n 25-2781-1,acft model b52. aluminum alloy, qq-a-250/13, alloy alclad 7075, 0, stock size 10.000in. lg, 3.500 in. w, 0.040 in. thk, bracket p/n 25-2781-11, clip p/N29-2498-12, clip p/n 29-2498-21
00-307-3076
Aircraft Skin
Used on aircraft,kc-135. 28.100" overall length 16.300" overall width
00-307-3077
Aircraft Former
47.160" overall length 0.313" material thickness
00-307-3079
Aircraft Former
47.160" overall length 0.310" material thickness
00-307-3082
Structural Component Air Support
Used on 65-6703-3,model kc135. consists of 1 support part no. 65-6703-8, 1 journal caps part no. 65-6703-3008
00-307-3165
Structural Component Air Support
14.540" overall length 1.640" overall width support, cover
00-307-3216
Aircraft Former
Used on aircraft,c-130a. 0.064" material thickness
